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	Design and Analysis of Radiometric Calibration Mission in-orbit for Environment and Disasters Monitoring Satellite 会议论文 OAI收割 Yokohama, Japan, 2019-07-28 作者: Zhu, Yang; Zhu, Jun; Bai, Zhaoguang; Dong, Jun; Wu, Bin \| 收藏 \| 浏览/下载：49/0 \| 提交时间：2020/03/10 environment and disasters monitoring in-orbit radiometric calibration side-slither calibration along track scanning satellite attitude stability
	A STUDY ON IN-ORBIT CALIBRATION FOR A SPACEBORNE DISTRIBUTED INTERFEROMETER 会议论文 OAI收割 Valencia, SPAIN, JUL 22-27, 2018 作者: Lan, Ailan; Yan, Jingye; Wu, Lin; Zhao, Fei; Wu, Ji \| 收藏 \| 浏览/下载：26/0 \| 提交时间：2019/01/31 in-orbit calibration discrepancy inter-satellite distance spaceborne distributed interferometer
	In-orbit instrument performance study and calibration for POLAR polarization measurements 期刊论文 OAI收割 NUCLEAR INSTRUMENTS & METHODS IN PHYSICS RESEARCH SECTION A-ACCELERATORS SPECTROMETERS DETECTORS AND ASSOCIATED EQUIPMENT, 2018, 卷号: 900, 页码: 8-24 作者: Szabelski, J; Shi, HL; Rybka, DK; Pohl, M; Marcinkowski, R \| 收藏 \| 浏览/下载：46/0 \| 提交时间：2019/09/24 POLAR In-orbit calibration X-ray polarization Gamma-ray burst Monte Carlo simulation
	DEVELOPMENT OF THE RECONSTRUCTIVE TRANSPONDER FOR IN-ORBIT CALIBRATION OF HY-2 ALTIMETER 会议论文 OAI收割 IEEE International Geoscience and Remote Sensing Symposium (IGARSS), Milan, ITALY, JUL 26-31, 2015 作者: Wang, Caiyun; Guo, Wei; Zhao, Fei; Wan, Junzhi; Xu, Ke 收藏 \| 浏览/下载：18/0 \| 提交时间：2016/04/22 HY-2 altimeter in-orbit calibration transponder signal reconstructive clock drift
	ACMR SYSTEM DESCRIPTION AND PERFORMANCE 会议论文 OAI收割 IEEE International Geoscience and Remote Sensing Symposium (IGARSS), Quebec, CANADA, JUL 13-18, 2014 作者: Zhang, Dehai; Wang, Zhenzhan; Wang, Hongjian; Zhao, Jin; Li, Yun 收藏 \| 浏览/下载：25/0 \| 提交时间：2015/09/18 ACMR Calibration In-orbit performance
	Design and calibration of the solar irradiance monitor (EI CONFERENCE) 会议论文 OAI收割 International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China 作者: Yang D.-J.; Gong C.-H.; Wang Y.-P.; Ye X.; Fang W. 收藏 \| 浏览/下载：25/0 \| 提交时间：2013/03/25 The solar irradiance monitor (SIM) with the design accuracy of 5 used to monitor the secular changes of the total solar irradiance on FY-3 satellite takes the sun-scanning measurement method on-orbit. Compared to the sun-tracking measurement method this method simplifies the structure and cuts the cost but the measuring accuracy is affected by the sun-synchronous orbit sunlight incidence angle and the installing angle of the SIM in the satellite. Through the ground calibration experiment studies on the affection of different sunlight incidence angles to the measurement accuracy. First by the satellite tool kit (STK) simulation software simulates the orbital parameters of the sun-synchronous satellite and calculates the Sun ascension and declination at any time. By the orbit coordinate transformation matrix gets the components of the Sun vectors to the axes of the satellite and base on the components designs the field of view and the installing angles of the SIM. Then designs and completes the calibration experiment to calibrate the affection of the incidence angles. Selecting 11 different angles between the sunlight and the satellite X-axis measures the total solar irradiance by the SIM at each angle and compares to the irradiances of the SIAR reference radiometers and gets the coefficient curves of the three channels of the SIM. Finally by the quadratic fitting gets the correction equations on the incidence angles: R 1=5.7110-52 -2.45310 -3+1.0302 R2=2.8410-5-1. 96510-3+1.0314 and R3 =1.7210 -52-4.18410-4+0.9946. The equations will aimprove the on-orbit measurement accuracy of the solar irradiance and are very important to the on-orbit data processing after the satellite launched. 2011 SPIE.
	The Simulation measurement experiment and calibration for Solar Total Irradiance Monitor on board (EI CONFERENCE) 会议论文 OAI收割 ICO20: Remote Sensing and Infrared Devices and Systems, August 21, 2005 - August 26, 2005, Changchun, China Yupeng W.; Wei F.; Bingxi Y. 收藏 \| 浏览/下载：37/0 \| 提交时间：2013/03/25 STIM (Solar Total Irradiance Monitor) can be used on sun-synchronous polar orbit weather satellites to measure the total solar irradiance. It contains three independent and identical wide view absolute radiometers. They are mounted on the satellite in an angle which ensure the sun scan over the field of view of the absolute radiometers. This measurement method doesn't need the instrument tracking the sun but the sun scan over the field of view of the absolute radiometers in each orbit cycle. The paper presents the measurement method of simulation for solar irradiance measurement and calibration by mounting the instrument on a two-axis rotation table. By controlling the rotation angle velocity of the instrument in the meridian direction being the same as that of the weather satellite's on orbit we can measure the solar irradiance when the sun scan over the field of view of the absolute radiometers to simulate the onboard state. And we have operated the measurement with the prototype of STIM. The SIAR-1 is traceable to WRR and serves as a transfer standard. So simultaneous comparison measurements between SIAR-1 and each of the three wide view absolute radiometers are measured to provide calibration corrections to the instrument. And we have a further study at the influence of stray light to the measurement results. This paper presents the method of simulation experiment and calibration for solar irradiance measurement with Solar Total Irradiance Monitor on board.